关闭×
Home
|
About Journal
|
Editorial Board
|
Instruction
|
Publication Ethics Statement
|
Subscriptions
|
Contacts Us
|
Chinese
Office Online
Submission Online
Peer Review
Editor Work
Editor-in-chief
Office Work
Journal Online
Accepted
Current Issue
Advanced Search
Archive
Read Articles
Download Articles
Email Alert
Quick Search
Adv Search
2010 Vol. 53, No. 10
Published: 2010-05-15
FEATURE
FIGURE
FORUM
NEW VIEWPOINT
RESEARCH
COVER STORY
FEATURE
26
Current Situation and Prospect of Key Technologies of Domestic NC Machine Tool
DOI: 10.16080/j.issn1671-833x.2010.10.013
2010 Vol. 53 (10): 26-30 [
Abstract
] (
70
)
HTML
New
PDF
(1437 KB) (
1624
)
COVER STORY
34
Ready for Take off
DOI: 10.16080/j.issn1671-833x.2010.10.021
2010 Vol. 53 (10): 34-37 [
Abstract
] (
64
)
HTML
New
PDF
(2060 KB) (
175
)
FORUM
40
Research Progress of Open Type Intelligent NC Machine Tool
DOI: 10.16080/j.issn1671-833x.2010.10.014
2010 Vol. 53 (10): 40-44 [
Abstract
] (
58
)
HTML
New
PDF
(1706 KB) (
377
)
45
Development Trend and Key Technologies of NC Machine Tool for Aviation Industry
DOI: 10.16080/j.issn1671-833x.2010.10.005
2010 Vol. 53 (10): 45-48 [
Abstract
] (
62
)
HTML
New
PDF
(1266 KB) (
368
)
49
Advanced Technology of NC Machine Tool
DOI: 10.16080/j.issn1671-833x.2010.10.015
2010 Vol. 53 (10): 49-52 [
Abstract
] (
66
)
HTML
New
PDF
(1967 KB) (
459
)
54
Development and Current Research of NC Combined Grinding Technology
DOI: 10.16080/j.issn1671-833x.2010.10.016
2010 Vol. 53 (10): 54-57 [
Abstract
] (
66
)
HTML
New
PDF
(1348 KB) (
492
)
NEW VIEWPOINT
58
Flexible Tooling Technology and Application for Digital Assembly of Aircraft Panel Component
DOI: 10.16080/j.issn1671-833x.2010.10.006
2010 Vol. 53 (10): 58-61 [
Abstract
] (
70
)
HTML
New
PDF
(1632 KB) (
559
)
RESEARCH
64
Finite Element Analysis on Head Forming Process of Ti-6Al-4V Hexagon Bolt
DOI: 10.16080/j.issn1671-833x.2010.10.001
Bolt head used in aviation industry is various and very complex, and usually formed by forging. By using a simulation software, the head forming process of Ti-6Al-4V hexagon bolt is simulated, and the stress field, strain field, temperature field and material flow are analyzed. Meanwhile the possible faults like folding and crack are predicted, which can offer theory basis for the design and improvement of the process.
2010 Vol. 53 (10): 64-68/87 [
Abstract
] (
60
)
HTML
New
PDF
(1944 KB) (
185
)
69
Permeability of Preform With Resin
DOI: 10.16080/j.issn1671-833x.2010.10.002
An experimental investigation is carried out to deal with the permeability of preform with resin by applying the unidirectional saturated flow method. Several factors which affect the permeability are studied, including the rate of resin in preform, the ply stacking sequence, the injection pressure and the temperature. The results indicate that the rate of resin in preform influence the permeabiliy, and the laws for different ply stacking sequence are not the same. For glass fabric of (0,90), the permeability increases first, then decreases, and finally increases as the increasing of resin. The injection pressure and the temperature do not have remarkable effect on the permeability.
2010 Vol. 53 (10): 69-71/91 [
Abstract
] (
60
)
HTML
New
PDF
(1339 KB) (
191
)
72
Development of FL-9 Wind Tunnel Model Support Carriage Based on Virtual Design and Manufacturing Technology
DOI: 10.16080/j.issn1671-833x.2010.10.007
2010 Vol. 53 (10): 72-75/84 [
Abstract
] (
66
)
HTML
New
PDF
(1579 KB) (
388
)
76
Rapid Generation of Two-Dimensional Drafting of Turbine Blade Body Profile Cross Section Line
DOI: 10.16080/j.issn1671-833x.2010.10.012
To realize the drafting of the turbine blade body profile cross section line rapidly, with turbine blade structure characteristic being united, the characteristic of cross section line should be abstracted before generating the drafting. Taking some type of the turbine blade as the concrete example, the process of abstracting characteristic, drafting generating and automatic table dimensioning of the data leading-in generated exterior cross section line are introduced. The method of abstracting characteristic of exterior cross section of arbitrarily altitude of turbine blade is expounded in detail.
2010 Vol. 53 (10): 76-79/84 [
Abstract
] (
57
)
HTML
New
PDF
(1458 KB) (
136
)
80
Evaluation of Interior Environment Design of Aircraft Passenger Cabin Based on Fuzzy-AHP
DOI: 10.16080/j.issn1671-833x.2010.10.008
Based on establishing the evaluation index firstly, Fuzzy AHP synthesize evaluation method is used to realize the conversion of qualitative attributes to quantitative attributes, and the evaluation analytical model of interior environment design of airplane passenger cabin is constructed which overcome the subjective and randomness, and scientific assessment is achieved. Moreover, evaluation system software for aircraft passenger cabin is designed as demonstration.
2010 Vol. 53 (10): 80-84 [
Abstract
] (
60
)
HTML
New
PDF
(1565 KB) (
590
)
85
Methods of Establishing Aircraft Fuel ALIs Based on FTA&FMEA
DOI: 10.16080/j.issn1671-833x.2010.10.009
“Unsafe condition” is determined with four-element evaluation criteria, and the problem of flammability exposure time is settled with MonteCarlo method. When determining the service intervals, FTA,FMEA are used to develop safety assessment and find fault modes relating to “unsafe condition”, then calculation of reliability degree distribution and service intervals is achieved.
2010 Vol. 53 (10): 85-87 [
Abstract
] (
81
)
HTML
New
PDF
(1045 KB) (
270
)
88
Fault Diagnosis Method for Gyro in Double-Redundant Strapdown Control System
DOI: 10.16080/j.issn1671-833x.2010.10.010
Considering rocket double-redundant strapdown control system consisting of six twodimension-of-freedoms gyros, advantages of integrated hardware redundancy and analytical redundancy, an advanced method for gyro fault diagnosis is designed; by using neural network observer, not only the problem which the fault diagnosis method based on hardware redundancy could not solve is able to be solved, but also the weakness of traditional analytical redundancy method could be overcome; by gyros’ adaptive thresholds, the robustness of fault diagnosis is improved; and it achieves the recovery of a fault gyros’ data.
2010 Vol. 53 (10): 88-91 [
Abstract
] (
61
)
HTML
New
PDF
(1087 KB) (
197
)
92
Laser Welding Repairing Technology of Aircraft Ti-Alloy Structure
DOI: 10.16080/j.issn1671-833x.2010.10.011
On the basis of IPG’s 4kW fibre laser equipment, the effect of jointing interspace, equivalent welding line energy and other technology parameters on the TC4 alloy’s joint strength are researched. It is found that under the optimal parameters, the joint’s strength can reach 99.5% of the matrix’s strength, which can meet the demand of damage’s repairing of aircraft Ti-alloy structrue.
2010 Vol. 53 (10): 92-94 [
Abstract
] (
91
)
HTML
New
PDF
(1581 KB) (
265
)
Notices
·
'Aeronautical Manufacturing technology ' is included in EI database
·
China Science Citation Database (CSCD)
·
Chinese S&T Journal Citation Reports (CJCR)
·
World Journal Clout Index (WJCI) Report of Scientific and Technological Periodicals
·
Supported in China Science and Technology Journal Excellence Action Plan
·
Aeronautical Manufacturing Technology ranked No. 3 in Chinese S&T Journal Citation Reports (CJCR)
·
High Quality Sci-tech Journal Classification Catalogue in Aerospace Field （2023）
·
A Guide to the Core Journals of China (hosted by Peking University Library)
Download
Copyright Transfer Agreement
Links
AVIC Manufacturing Technology Institute
AVIC
Copyright © Editorial Board of Aeronautical Manufacturing Technology
Supported by:
Beijing Magtech
